Method and system for detecting dynamic strain

ABSTRACT

A system and method for detecting dynamic strain of a housing. The system includes an optical fiber linearly affixed along a surface of a length of the housing and an interrogator comprising a laser source and a photodetector. The optical fiber comprises at least one pair of fiber Bragg gratings (FBGs) tuned to reflect substantially identical wavelengths with a segment of the optical fiber extending between the FBGs. The segment of the optical fiber is linearly affixed along the surface of the housing. The interrogator is configured to perform interferometry by shining laser light along the optical fiber and detecting light reflected by the FBGs. The interrogator outputs dynamic strain measurements based on interferometry performed on the reflected light.

CROSS-REFERENCE TO RELATED APPLICATIONS

This application is a continuation of U.S. patent application Ser. No.17/243,142, filed Apr. 28, 2021, which is a U.S. patent application Ser.No. 16/271,623, filed Feb. 8, 2019, now U.S. Pat. No. 11,313,744, whichis a continuation of U.S. patent application Ser. No. 15/323,937, filedJan. 4, 2017, now U.S. Pat. No. 10,234,345, which is the U.S. NationalStage of International Application No. PCT/CA2014/050645, filed Jul. 4,2014, all of which applications are incorporated by reference herein intheir entirety.

TECHNICAL FIELD

The present disclosure is directed at methods, systems, and techniquesfor detecting dynamic strain.

BACKGROUND

In a variety of industries, such as the oil and gas industry, the effectof dynamic strain on various components may be material for determiningwhether those components are functioning properly and for forecastingthe expected life of those components. Dynamic strain may also bemonitored for detecting failures in components such as well casing andpipelines. Research and development accordingly continue into methods,systems and techniques for detecting dynamic strain.

SUMMARY

According to a first aspect, there is provided a system for detectingdynamic strain of a housing. The system comprises an optical fiberlinearly affixed along a surface of a length of the housing and aninterrogator. The optical fiber comprises at least one pair of fiberBragg gratings (FBGs) tuned to reflect substantially identicalwavelengths with a segment of the optical fiber extending between theFBGs. The segment of the optical fiber is linearly affixed along thesurface of the housing. The interrogator comprises a laser source and aphotodetector. The interrogator is configured to perform interferometryby shining laser light along the optical fiber and detecting lightreflected by the FBGs. The interrogator outputs dynamic strainmeasurements based on interferometry performed on the reflected light.

The system may further comprise a signal processing device communicativewith the interrogator. The signal processing device may be configured toprocess the dynamic strain measurements to estimate where along thehousing the dynamic strain is occurring. The signal processing devicemay be configured to process the dynamic strain measurements to estimatemagnitude of the dynamic strain. The signal processing device may beconfigured to process the dynamic strain measurements and monitorchanges in frequency of dynamic strain.

The optical fiber may comprise first and second pairs of the FBGs. TheFBGs of the first pair may be tuned to a first wavelength and the FBGsof the second pair may be tuned to a second wavelength different fromthe first wavelength. The segments of the optical fiber between thefirst pair of FBGs and the second pair of FBGs may be linearly affixedalong the surface of different lengths of the housing. The interrogatormay be configured to use wavelength division multiplexing to measuredynamic strain at the different lengths of the housing.

The optical fiber may be linearly affixed directly to the surface of thelength of the housing. A plurality of fasteners may be used to affix theoptical fiber directly to the surface of the length of the housing. Thesurface of the length of the housing may comprises a longitudinallyextending linear groove in which the optical fiber is positioned. Acoating material may coat the optical fiber positioned in the lineargroove.

The optical fiber may be linearly affixed to a lining on the surface ofthe length of the housing. A plurality of fasteners may be used tolinearly affix the optical fiber to the lining. The lining may comprisea longitudinally extending linear groove in which the optical fiber ispositioned. A coating material may coat the optical fiber positioned inthe linear groove.

The optical fiber may be enclosed in a protective shell. The protectiveshell may comprise a metal tube.

The housing may be a conduit. Alternatively, the housing may be avessel.

According to another aspect, there is provided a method for detectingdynamic strain of a housing. the method comprises: shining laser lightalong an optical fiber linearly affixed along a surface of a length ofthe housing, wherein the optical fiber comprises at least one pair offiber Bragg gratings (FBGs) tuned to reflect substantially identicalwavelengths with a segment of the optical fiber extending between theFBGs, wherein the segment of the optical fiber is linearly affixed alongthe surface of the housing; and detecting light reflected by the FBGsand performing interferometry on the reflected light to produce dynamicstrain measurements based on the interferometry.

The method may further comprises processing the measurements to estimatewhere along the housing the dynamic strain is occurring.

The method may further comprises processing the measurements to estimatemagnitude of the dynamic strain.

The method may further comprises processing the measurements to monitorchanges in frequency of the dynamic strain.

According to another aspect, there is provided a system for detectingdynamic strain. The system comprises: an optical fiber comprising atleast one pair of fiber Bragg gratings (FBGs) tuned to reflectsubstantially identical wavelengths with a segment of the optical fiberlinearly extending between the FBGs; and an interrogator comprising alaser source and a photodetector. The interrogator is configured toperform interferometry by shining laser light along the optical fiberand detecting light reflected by the FBGs, and the interrogator outputsdynamic strain measurements based on interferometry performed on thereflected light.

The interrogator may comprise an optical source and a photodetector andmay be configured to: shine a reference light pulse and a sensing lightpulse along the optical fiber and control timing of the light pulsessuch that the reference light pulse is delayed compared to the sensinglight pulse by a predetermined period of time selected such that thereference light pulse reflected by a first FBG of the pair of FBGsinterferes with the sensing light pulse reflected by a second FBG of thepair of FBGs to form a combined interference pulse; detect a phasedifference between the reflected reference light pulse and the reflectedsensing light pulse of the combined interference pulse; and produce anoutput signal based on the phase difference detected.

The system may further comprise a signal processing device communicativewith the interrogator. The signal processing device may be configured toprocess the dynamic strain measurements to estimate where the dynamicstrain is occurring. The signal processing device may be configured toprocess the dynamic strain measurements to estimate magnitude of thedynamic strain. The signal processing device may be configured toprocess the dynamic strain measurements and monitor changes in frequencyof dynamic strain.

The optical fiber may comprise first and second pairs of the FBGs. TheFBGs of the first pair may be tuned to a first wavelength and the FBGsof the second pair may be tuned to a second wavelength different fromthe first wavelength. The interrogator may be configured to usewavelength division multiplexing to measure dynamic strain.

The optical fiber may be enclosed in a protective shell. The protectiveshell may comprise a metal tube.

According to another aspect, there is provided a method for detectingdynamic strain, comprising: shining laser light along an optical fiber,wherein the optical fiber comprises at least one pair of fiber Bragggratings (FBGs) tuned to reflect substantially identical wavelengthswith a segment of the optical fiber linearly extending between the FBGs;and detecting light reflected by the FBGs and performing interferometryon the reflected light to produce dynamic strain measurements based onthe interferometry.

The shining laser light step may comprise shining a reference lightpulse and a sensing light pulse along the optical fiber, the referencelight pulse being delayed compared to the sensing light pulse by apredetermined period of time selected such that the reference lightpulse reflected by a first FBG of the pair of FBGs interferes with thesensing light pulse reflected by a second FBG of the pair of FBGs toform a combined interference pulse. The detecting light reflected by theFBGs and performing interferometry step may comprise detecting thecombined interference pulse and detecting a phase difference between thereflected reference light pulse and the reflected sensing light pulse ofthe combined interference pulse to produce the dynamic strainmeasurements.

The method may further comprise processing the measurements to estimatewhere the dynamic strain is occurring.

The method may further comprise processing the measurements to estimatemagnitude of the dynamic strain.

The method may further comprise processing the measurements to monitorchanges in frequency of the dynamic strain.

The optical fiber may be deployed within a housing. The housing may beproduction tubing of a wellbore. Alternatively the housing may be apipeline.

According to another aspect, there is provided a method for detectingdynamic strain in a housing, comprising: shining a reference light pulseand a sensing light pulse along an optical fiber deployed within thehousing, wherein the optical fiber comprises at least one pair of fiberBragg gratings (FBGs) tuned to reflect substantially identicalwavelengths with a segment of the optical fiber extending between theFBGs, wherein the reference light pulse is delayed compared to thesensing light pulse by a predetermined period of time selected such thatthe reference light pulse reflected by a first FBG of the pair of FBGsinterferes with the sensing light pulse reflected by a second FBG of thepair of FBGs to form a combined interference pulse; and detecting thecombined interference pulse and detecting a phase difference between thereflected reference light pulse and the reflected sensing light pulse ofthe combined interference pulse to produce dynamic strain measurementsbased on the phase difference detected.

The housing may be production tubing of a wellbore. Alternatively, thehousing may be a pipeline.

This summary does not necessarily describe the entire scope of allaspects. Other aspects, features and advantages will be apparent tothose of ordinary skill in the art upon review of the followingdescription of specific embodiments.

BRIEF DESCRIPTION OF THE DRAWINGS

In the accompanying drawings, which illustrate one or more exemplaryembodiments:

FIG. 1A is a block diagram of a system for detecting dynamic strain,which includes an optical fiber with fiber Bragg gratings (“FBGs”) forreflecting a light pulse, according to one embodiment.

FIG. 1B is a schematic that depicts how the FBGs reflect a light pulse.

FIG. 1C is a schematic that depicts how a light pulse interacts withimpurities in an optical fiber that results in scattered laser light dueto Rayleigh scattering, which is used for distributed acoustic sensing(“DAS”).

FIG. 2A is a perspective view of a conduit with an optical fiberlinearly affixed to an outer surface of the conduit for detectingdynamic strain of the conduit according to one embodiment.

FIG. 2B is a perspective view of a conduit with multiple optical fiberslinearly affixed in parallel alignment to an outer surface of theconduit for detecting dynamic strain of the conduit according to oneembodiment.

FIG. 3 is a perspective view of a conduit with a lining surrounding theconduit and an optical fiber linearly affixed to the lining fordetecting dynamic strain of the conduit according to one embodiment.

FIG. 4 depicts a graph of cumulative dynamic strain at various locationsalong a housing vs. time.

FIG. 5 depicts a graph of magnitude of dynamic strain vs. time forsegments of an optical fiber (channels 1-4) linearly affixed along anexternal surface of a conduit, each of the segments of the optical fiberextending linearly between a pair of FBGs (channels 1-4).

FIG. 6 is a schematic of a system for detecting dynamic strain in awellbore using the optical fiber with FBGs according to one embodiment.

DETAILED DESCRIPTION

Directional terms such as “top,” “bottom,” “upwards,” “downwards,”“vertically,” and “laterally” are used in the following description forthe purpose of providing relative reference only, and are not intendedto suggest any limitations on how any article is to be positioned duringuse, or to be mounted in an assembly or relative to an environment.

Optical interferometry is a technique in which two separate light pulsesare generated: a sensing pulse and a reference pulse. These pulses maybe generated by an optical source such as a laser. When opticalinterferometry is used for fiber optic sensing applications, the sensingand reference pulses are at least partially reflected back towards anoptical receiver. As described in further detail below, opticalinterferometry may be used to detect dynamic strain.

Referring now to FIG. 1A, there is shown one embodiment of a system 100for detecting dynamic strain. The system 100 comprises the optical fiber112, an interrogator 106 optically coupled to the optical fiber 112, anda signal processing device 118 that is communicative with theinterrogator 106. While not shown in FIG. 1A, within the interrogator106 are an optical source, optical receiver, and an optical circulator.The optical circulator directs light pulses from the optical source tothe optical fiber 112 and directs light pulses received by theinterrogator 106 from the optical fiber 112 to the optical receiver.

The optical fiber 112 comprises one or more fiber optic strands, each ofwhich is made from quartz glass (amorphous SiO₂). The fiber opticstrands are doped with a rare earth compound (such as germanium,praseodymium, or erbium oxides) to alter their refractive indices,although in alternative embodiments the fiber optic strands may not bedoped. Single mode and multimode optical strands of fiber arecommercially available from, for example, Corning® Optical Fiber.Example optical fibers include ClearCurve™ fibers (bend insensitive),SMF28 series single mode fibers such as SMF-28 ULL fibers or SMF-28efibers, and InfiniCor® series multimode fibers.

The interrogator 106 generates the sensing and reference pulses andoutputs the reference pulse after the sensing pulse. The pulses aretransmitted along optical fiber 112 that comprises a first pair of fiberBragg gratings (“FBGs”). The first pair of FBGs comprises first andsecond FBGs 114 a,b (generally, “FBGs 114”). The first and second FBGs114 a,b are separated by a certain segment 116 of the optical fiber 112(“fiber segment 116”). The optical length of the fiber segment 116varies in response to dynamic strain that the optical fiber 112experiences.

The light pulses have a wavelength identical or very close to the centerwavelength of the FBGs 114, which is the wavelength of light the FBGs114 are designed to partially reflect; for example, typical FBGs 114 aretuned to reflect light in the 1,000 to 2,000 nm wavelength range. Thesensing and reference pulses are accordingly each partially reflected bythe FBGs 114 a,b and return to the interrogator 106. The delay betweentransmission of the sensing and reference pulses is such that thereference pulse that reflects off the first FBG 114 a (hereinafter the“reflected reference pulse”) arrives at the optical receiver 103simultaneously with the sensing pulse that reflects off the second FBG114 b (hereinafter the “reflected sensing pulse”), which permits opticalinterference to occur.

While FIG. 1A shows only the one pair of FBGs 114 a,b, in alternativeembodiments (not depicted) any number of FBGs 114 may be on the fiber112, and time division multiplexing (TDM) (and optionally, wavelengthdivision multiplexing (WDM)) may be used to simultaneously obtainmeasurements from them. If two or more pairs of FBGs 114 are used, anyone of the pairs may be tuned to reflect a different center wavelengththan any other of the pairs. Alternatively a group of multiple FBGs 114may be tuned to reflect a different center wavelength to another groupof multiple FBGs 114 and there may be any number of groups of multipleFBGs extending along the optical fiber 112 with each group of FBGs 114tuned to reflect a different center wavelength. In these exampleembodiments where different pairs or group of FBGs 114 are tuned toreflect different center wavelengths to other pairs or groups of FBGs114, WDM may be used in order to transmit and to receive light from thedifferent pairs or groups of FBGs 114, effectively extending the numberof FBG pairs or groups that can be used in series along the opticalfiber 112 by reducing the effect of optical loss that otherwise wouldhave resulted from light reflecting from the FBGs 114 located on thefiber 112 nearer to the optical source 101. When different pairs of theFBGs 114 are not tuned to different center wavelengths, TDM issufficient.

The interrogator 106 emits laser light with a wavelength selected to beidentical or sufficiently near the center wavelength of the FBGs 114that each of the FBGs 114 partially reflects the light back towards theinterrogator 106. The timing of the successively transmitted lightpulses is such that the light pulses reflected by the first and secondFBGs 114 a,b interfere with each other at the interrogator 106, and theoptical receiver 103 records the resulting interference signal. Thestrain that the fiber segment 116 experiences alters the optical pathlength between the two FBGs 114 and thus causes a phase difference toarise between the two interfering pulses. The resultant optical power atthe optical receiver 103 can be used to determine this phase difference.Consequently, the interference signal that the interrogator 106 receivesvaries with the strain the fiber segment 116 is experiencing, whichallows the interrogator 106 to estimate the strain the fiber segment 116experiences from the received optical power. The interrogator 106digitizes the phase difference (“output signal”) whose magnitude andfrequency vary directly with the magnitude and frequency of the dynamicstrain the fiber segment 116 experiences.

The signal processing device 118 is communicatively coupled to theinterrogator 106 to receive the output signal. The signal processingdevice 118 includes a processor 102 and a non-transitory computerreadable medium 104 that are communicatively coupled to each other. Aninput device 110 and a display 108 interact with the processor 102. Thecomputer readable medium 104 has encoded on it statements andinstructions to cause the processor 102 to perform any suitable signalprocessing methods to the output signal. For example, if the fibersegment 116 is laid adjacent a region of interest that is simultaneouslyexperiencing vibration at a rate under 20 Hz and acoustics at a rateover 20 Hz, the fiber segment 116 will experience similar strain and theoutput signal will comprise a superposition of signals representative ofthat vibration and those acoustics. The processor 102 may apply a lowpass filter with a cutoff frequency of 20 Hz to the output signal toisolate the vibration portion of the output signal from the acousticsportion of the output signal. Analogously, to isolate the acousticsportion of the output signal from the vibration portion, the processor102 may apply a high pass filter with a cutoff frequency of 20 Hz. Theprocessor 102 may also apply more complex signal processing methods tothe output signal; example methods include those described in PCTapplication PCT/CA2012/000018 (publication number WO 2013/102252), theentirety of which is hereby incorporated by reference.

FIG. 1B depicts how the FBGs 114 reflect the light pulse, according toanother embodiment in which the optical fiber 112 comprises a third FBG114 c. In FIG. 1B, the second FBG 114 b is equidistant from each of thefirst and third FBGs 114 a,c when the fiber 112 is not strained. Thelight pulse is propagating along the fiber 112 and encounters threedifferent FBGs 114, with each of the FBGs 114 reflecting a portion 115of the pulse back towards the optical receiver 101. In embodimentscomprising three or more FBGs 114, the portions of the sensing andreference pulses not reflected by the first and second FBGs 114 a,b canreflect off the third FBG 114 c and any subsequent FBGs 114, resultingin interferometry that can be used to detect strain along the fiber 112occurring further from the optical source 101 than the second FBG 114 b.For example, in the embodiment of FIG. 1B, a portion of the sensingpulse not reflected by the first and second FBGs 114 a,b can reflect offthe third FBG 114 c and a portion of the reference pulse not reflectedby the first FBG 114 a can reflect off the second FBG 114 b, and thesereflected pulses can interfere with each other at the interrogator 106.

Any changes to the optical path length of the fiber segment 116 resultin a corresponding phase difference between the reflected reference andsensing pulses at the interrogator 106. Since the two reflected pulsesare received as one combined interference pulse, the phase differencebetween them is embedded in the combined signal. This phase informationcan be extracted using proper signal processing techniques, such asphase demodulation. The relationship between the optical path of thefiber segment 116 and that phase difference (θ) is as follows:

$\theta = \frac{2\pi{nL}}{\lambda}$

where n is the index of reaction of the optical fiber; L is the opticalpath length of the fiber segment 116; and is the wavelength of theoptical pulses. A change in nL is caused by the fiber experiencinglongitudinal strain induced by energy being transferred into the fiber.The source of this energy may be, for example, an object outside of thefiber experiencing dynamic strain, undergoing vibration, or emittingenergy. As used herein, “dynamic strain”, refers to strain that changesover time. Dynamic strain that has a frequency of between about 5 Hz andabout 20 Hz is referred to by persons skilled in the art as “vibration”,dynamic strain that has a frequency of greater than about 20 Hz isreferred to by persons skilled in the art as “acoustics”, and dynamicstrain that changes at a rate of <1 Hz, such as at 500 μHz, is referredto as “sub-Hz strain”.

One conventional way of determining ΔnL is by using what is broadlyreferred to as distributed acoustic sensing (“DAS”). DAS involves layingthe fiber 112 through or near a region of interest and then sending acoherent laser pulse along the fiber 112. As shown in FIG. 1C, the laserpulse interacts with impurities 113 in the fiber 112, which results inscattered laser light 117 because of Rayleigh scattering. Vibration oracoustics emanating from the region of interest results in a certainlength of the fiber becoming strained, and the optical path change alongthat length varies directly with the magnitude of that strain. Some ofthe scattered laser light 117 is back scattered along the fiber 112 andis directed towards the optical receiver 103, and depending on theamount of time required for the scattered light 117 to reach thereceiver and the phase of the scattered light 117 as determined at thereceiver, the location and magnitude of the vibration or acoustics canbe estimated with respect to time. DAS relies on interferometry usingthe reflected light to estimate the strain the fiber experiences. Theamount of light that is reflected is relatively low because it is asubset of the scattered light 117. Consequently, and as evidenced bycomparing FIGS. 1B and 1C, Rayleigh scattering transmits less light backtowards the optical receiver 103 than using the FBGs 114.

DAS accordingly uses Rayleigh scattering to estimate the magnitude, withrespect to time, of the strain experienced by the fiber during aninterrogation time window, which is a proxy for the magnitude of thevibration or acoustics emanating from the region of interest. Incontrast, the embodiments described herein measure dynamic strain usinginterferometry resulting from laser light reflected by FBGs 114 that areadded to the fiber 112 and that are designed to reflect significantlymore of the light than is reflected as a result of Rayleigh scattering.This contrasts with an alternative use of FBGs 114 in which the centerwavelengths of the FBGs 114 are monitored to detect any changes that mayresult to it in response to strain. In the depicted embodiments, groupsof the FBGs 114 are located along the fiber 112. A typical FBG can havea reflectivity rating of 2% or 5%. The use of FBG-based interferometryto measure dynamic strain offers several advantages over DAS, in termsof optical performance.

In some of the presently disclosed embodiments, optical fiber 112 islinearly affixed along a surface of a length of housing to detectdynamic strain of the housing. The optical fiber 112 including fibersegments 116 positioned between pairs of FBGs 114 longitudinally extendsalong the surface of the housing with the fiber segments 116 linearlyaffixed along the housing surface. When the housing is subjected todynamic strain caused by vibration or sound, this results incorresponding strain or pull on the fiber segments 116. The opticallength of the fiber segment 116 varies in response to the amount ofstrain the fiber 112 is experiencing and thus changes the interferencepattern produced by the FBGs 114 and recorded by the interrogator 106 asdiscussed above in more detail. The fiber 112 may be linearly affixedalong substantially the whole length of the housing or a portionthereof. The fiber 112 may be linearly affixed to the external orinternal surface of the housing. The fiber 112 may be in direct contactwith the housing surface or it may be on or embedded in some sort oflining or carrier on the internal or external surface of the housing.The housing surface may comprise a longitudinally extending lineargroove along a length of the housing surface and the optical fiber 112may be positioned in the groove. A protective coating or filler may beprovided over the optical fiber 112 to fill any space within the grooveand to protect the fiber from damage. Alternatively the optical fiber112 may be enclosed in a protective shell for example a metal tube suchas a stainless steel tube. The optical fiber 112 (optionally enclosed inthe protective shell) may be linearly affixed to the housing or liningby a plurality of fasteners, such as zip or cable ties, tape, cableclips, cable mounts or the like.

As the optical fiber 112 is linearly affixed along a surface of thehousing, the optical fiber 112 may be enclosed in a protective shellsuch as a stainless steel tube as described above and the protectiveshell may be of a thickness and stiffness that reduces or does notpermit bending of the optical fiber 112 in order to protect the opticalfiber 112. In one example embodiment, the optical fiber 112 is enclosedwithin a ¼ inch stainless steel tubing.

The housing may be a vessel, such as a fluid storage vessel.Alternatively the housing may be a conduit of any cross-sectional shapeor size, for example a tubular, pipeline, or the like through whichfluid flows. A fiber optic cable may be positioned inside the conduitfor sensing conditions within the conduit. For example, the fiber opticcable may be made up of a plurality of fiber optic strands which mayinclude a distributed temperature sensing (“DTS”) transmission line asis known in the art and described in US 2009/0326826 (incorporatedherein by reference).

Dynamic strain may be monitored using the system and method of thedisclosed embodiments to provide an indication that fluid is leakingfrom the housing. Dynamic strain may also be monitored to identifyhotspots in a housing, which hotspots are experiencing strain over timeand are more likely to fail. In addition, dynamic strain may bemonitored for many other applications such as geosteering, pipelinecollision detection, and pig tracking as is known in the art.

Referring now to FIGS. 2A and 2B there are shown embodiments of aconduit 120 with longitudinally extending optical fiber 112 linearlyaffixed along the outer surface of the conduit 120. The optical fiber112 is in direct contact with the conduit 120. The optical fiber 112 islinearly affixed along substantially the entire length of the conduit120, however in alternative embodiments (not shown) the optical fiber112 may be linearly affixed along a portion of the length of the conduit120. The optical fiber 112 is linearly affixed along the outer surfaceof the conduit 120, however in alternative embodiments (not shown) theoptical fiber 112 may be linearly affixed along the internal surface ofthe conduit 120. In FIG. 2A a single optical fiber 112 is linearlyaffixed along the outer surface of the conduit 120, whereas in FIG. 2Bmultiple optical fibers 112 are in longitudinal parallel alignmentaround the circumference of the conduit 120, with each optical fiber 112linearly affixed along the outer surface of the conduit 120. In analternative embodiment (not shown) multiple optical fibers 112 may belinearly affixed along the internal surface of the conduit 120 or otherhousing with the fibers 112 being in longitudinal parallel alignment.Provision of multiple optical fibers 112 positioned in longitudinalparallel alignment along the surface of the housing may provide morecomprehensive detection of dynamic strain from the area surrounding theinternal or internal surface of the housing as the dynamic strain willbe detected by optical fiber 112 in closest alignment with the source ofthe dynamic strain.

Referring now to FIG. 3 , there is shown an embodiment of a conduit 120with a lining or carrier 130 surrounding the conduit 120 and opticalfiber 112 linearly embedded in the lining 130. The lining 130 may beextruded over the conduit 120 or wrapped or laid around the externalsurface of the conduit 120 using methods known in the art.Alternatively, the lining 130 may be positioned on the internal surfaceof the conduit 120. The lining 130 includes a longitudinally extendinglinear groove in the outer surface of the lining 130. The groovereceives the optical fiber 112 and a protective filler or coating (notshown) may be coated over the fiber 112 to fill any spaces within thegroove. In an alternative embodiment (not shown), the filler may not beprovided. The depth of the groove is such that the fiber 112 is below orflush with the outer surface of the lining 130, which, together with theprotective coating 132, may beneficially protect the fiber 112 and mayprevent snagging of the fiber 112. In another alternative embodiment,the groove may not be provided on the surface of the lining 130 and theoptical fiber 112 may be linearly affixed directly to the lining surfaceor embedded in the lining 130 in some other way, such as extruding thelining 130 with the fiber 112.

The lining 130 may be made of a material that is able to transmitdynamic strain, so as not to hinder the fiber's ability to detectdynamic strain of the housing. The lining material selected should alsohave sufficient tensile strength to allow the material to be stretchedin response to dynamic strain without breaking or failing. Suitablematerials for the lining 130 include, but are not limited to, plastics,for example high temperature and formable plastics. The filler orcoating may be a formable or curable material, such as a formableplastic, or a thermoset, thermoplastic or UV cured elastomer, which canexpand to fill the groove. The filler material selected may have acoefficient of expansion corresponding to the coefficient of expansionof the lining material.

The system and method disclosed herein may be used to monitor changes infrequency of dynamic strain of the housing. Alternatively, oradditionally, the system may be used to monitor changes in magnitude ofdynamic strain of the housing. A change in magnitude of dynamic strainmay indicate stretch, compression, elongation or shear of the housing.The magnitude of dynamic strain may also indicate severity of the strainbeing applied to the housing, for example, the larger the strain beingapplied to the housing, the greater the magnitude of dynamic strain. Itfollows that the more severe the strain being applied at a particularlocation of the housing, the more likely the housing will be compromisedand fail in the future.

The system and method disclosed herein may be used to monitor cumulativestrain of the housing where the dynamic strain is monitored over time.FIG. 4 shows an exemplary graph of cumulative dynamic strain at variouslocations along a housing vs. time. The cumulative dynamic strainrepresented by the graph is measured using an optical fiber 112comprising pairs of FBGs 114 representing five sensor zones (zones 1-5).The sensor zones and time are given on the horizontal axes and thevertical axes shows the total accumulated strain (rads). For the firstfive seconds, the housing is under no strain. Strain is first applied tozone 1 (hence the initial rise in the cumulative strain in this zone).Then at about ten seconds, strain is applied to zone 5, resulting in anincrease in the accumulated strain in zone 5. No further strain isintroduced to the system, resulting in a leveling off of the accumulatedstrain graph. Strain is a unitless measurement and is relative ratherthan absolute. As such, the system may be calibrated and straincorrelated to a recognized measurement such as displacement or appliedforce or pressure. Cumulative strain can be used to provide anindication of when it is time for the operator to replace the housing bycomparing the cumulative strain to a predetermined reference value.

The system and method may be used to estimate where along the housingthe dynamic strain is occurring. This may be useful to provide anindication of where a leak is occurring, or is likely to occur, or forother uses as is known in the art such as monitoring steam injection ina nearby production well. FIG. 5 shows an exemplary graph of magnitudeof strain (radians) over time for different fiber segments 116 (channels1-4) of an optical fiber 112 linearly affixed along an external surfaceof a conduit. The greatest magnitude of strain is detected by thechannel 3 fiber segment with channel 2 fiber segment and channel 4 fibersegment positioned either side of channel 3 fiber segment having thenext largest magnitude of strain. Channel 1 fiber segment is furthestaway from channel 3 fiber segment and has the smallest magnitude ofstrain. This graph indicates that there is dynamic strain in thevicinity of where the channel 3 fiber segment is affixed to the housing.The dynamic strain may be a leak in the housing or something else thatcauses the dynamic strain such as steam injection in a nearby productionwell. This dynamic strain is transient causing a spike in the magnitudeof dynamic strain.

In other embodiments, the optical fiber 112 comprises at least one pairof FBGs 114 tuned to reflect substantially identical wavelengths withfiber segment 116 linearly extending between the FBGs 114. The opticalfiber 112 may comprise multiple pairs of FBGs 114 or groups of multipleFBGs 114 as described above with the fiber segments 116 linearlyextending between the FBGs 114. The optical fiber 112 may be enclosed ina protective shell for example a metal tube such as a stainless steeltube to protect the optical fiber 112. In these embodiments the opticalfiber 112 is used with interrogator 106 in a method and system to detectdynamic strain as described above.

The method and system may be used to detect and monitor dynamic strainof, or in, a variety of housings over large or small distances. Forexample the optical fiber 112 may be deployed in a housing for detectingdynamic strain in the housing. In addition, the optical fiber 112 may bepositioned outside the housing, for example within a few meters from theexterior surface of the housing. For example, the housing may be apipeline and the optical fiber 112 may be buried in the ground near thepipeline to detect acoustics of the pipeline. The optical fiber 112 maybe buried between two pipelines (for example equidistance between bothpipelines) and used to detect acoustics in both pipelines. The housingmay be a vessel, such as a fluid storage vessel. Alternatively, thehousing may be a conduit of any cross-sectional shape or size, forexample a tubular, pipeline, or casing of an oil and gas well. Themethod and system may also be used to detect and monitor dynamic strainof a physical area over large or small distances, for example aperimeter of a building, an oil and gas well, or any area, where theoptical fiber 112 is deployed in the physical area being monitored.

Dynamic strain may be monitored to provide an indication that fluid isleaking from a housing, such as a conduit or vessel. Dynamic strain mayalso be monitored to identify hotspots in a housing, which hotspots areexperiencing strain over time and are more likely to fail. Dynamicstrain may also be monitored for many other applications such asgeosteering, pipeline collision detection, and pig tracking as is knownin the art.

The system and method may be used to monitor changes in frequency ofdynamic strain of a housing. Alternatively, or additionally, the systemand method may be used to monitor changes in magnitude of dynamic strainof a housing. A change in magnitude of dynamic strain may indicatestretch, compression, elongation or shear of the housing. The magnitudeof dynamic strain may also indicate severity of the strain being appliedto the housing, for example, the larger the strain being applied to thehousing, the greater the magnitude of dynamic strain. It follows thatthe more severe the strain being applied at a particular location of thehousing, the more likely the housing will be compromised and fail in thefuture at that location. The method and system may be used to estimatewhere along the housing the dynamic strain is occurring. This may beuseful to provide an indication of where a leak is occurring, or islikely to occur, or for other uses as is known in the art.

Referring now to FIG. 6 , there is shown a schematic of a system 200 fordetecting dynamic strain within a wellbore, according to anotherembodiment. In FIG. 6 , a wellbore 234 is drilled into a formation 214that contains oil or gas deposits (not shown). Various casing and tubingstrings are then strung within the wellbore 234 to prepare it forproduction. In FIG. 6 , surface casing 216 is the outermost string ofcasing and circumscribes the portion of the interior of the wellbore 234shown in FIG. 6 . A string of production casing 218 with a smallerradius than the surface casing 216 is contained within the surfacecasing 216, and an annulus (unlabeled) is present between the productionand surface casings 218, 216. A string of production tubing 220 iscontained within the production casing 218 and has a smaller radius thanthe production casing 218, resulting in another annulus (unlabeled)being present between the production tubing and casing 220, 218. Thesurface and production casings 216, 218 and the production tubing 220terminate at the top of the wellbore 234 in a wellhead 232 through whichaccess to the interior of the production tubing 220 is possible.

Although the wellbore 234 in FIG. 6 shows only with the production andsurface casings 218, 216 and the production tubing 220, in alternativeembodiments (not shown) the wellbore 234 may be lined with more, fewer,or alternative types of tubing or casing. For example, in one suchalternative embodiment a string of intermediate casing may be present inthe annulus between the surface and production casings 216, 218. Inanother such alternative embodiment in which the wellbore 234 ispre-production, only the surface casing 216, or only the surface andproduction casings 216, 218, may be present.

FIG. 6 also shows four examples of leaks 228 a-d (collectively, “leaks228”) that result in dynamic strain. One of the leaks 228 a is of fluidcrossing the formation 214's surface. Another of the leaks 228 b is offluid crossing the surface casing 216, while a third leak 228 c is offluid crossing the production casing 218, and a fourth leak 228 d is offluid crossing the production tubing 220. Although not depicted in FIG.6 , fluid flowing into the formation 214 from the wellbore 234 can alsoconstitute a leak. As mentioned above, in alternative embodiments (notshown) the wellbore 234 may contain more, fewer, or other types ofcasing or tubing strings, and in such embodiments the leaks may resultfrom fluid crossing any or more of these strings.

Optical fiber 112 is lowered into the production tubing 220 by spoolingdevice 212. The optical fiber 112 comprises at least one pair of FBGs114 tuned to reflect substantially identical wavelengths with fibersegment 116 linearly extending between the FBGs 114. The optical fiber112 may comprise multiple pairs of FBGs 114 or groups of multiple FBGs114 as described above. The optical fiber 112 may be enclosed in aprotective shell for example a metal tube such as a stainless steel tubeto protect the optical fiber 112. At the end of the optical fiber 112 isa weight 222 to help ensure the optical fiber 112 is relatively tautduring well logging.

As described above, the interrogator 106 generates sensing and referencepulses which are transmitted along the optical fiber 112 that comprisesat least one pair of FBGs 114 separated by a fiber segment 116. Theoptical length of the fiber segment 116 varies in response to dynamicstrain that the optical fiber 112 experiences caused by leaks 228 a-d oranother source of dynamic strain. The sensing and reference pulses areeach partially reflected by the FBGs 114 and return to the interrogator106 resulting in interference of the reflected sensing and referencepulses as described above with reference to FIGS. 1A and 1B. Theinterference signal that the interrogator 106 receives varies with thestrain the fiber segment 116 is experiencing, which allows theinterrogator 106 to estimate the strain the fiber segment 116experiences from the received optical power. The interrogator 106digitizes the phase difference (“output signal”) whose magnitude andfrequency vary directly with the magnitude and frequency of the dynamicstrain the fiber segment 116 experiences. The signal processing device118 is communicatively coupled to the interrogator 106 to receive theoutput signal. The signal processing device 118 includes processor 102and computer readable medium 104 that are communicatively coupled toeach other as described above with reference to FIG. 1A. The signalprocessing device 118 processes the output signals received by theinterrogator 106 to provide an indication of where in the wellbore thedynamic strain is occurring and this information may be used toindentify leaks 228 a-d. Housing 202 positioned on the surface housesthe spooling device 212, interrogator 106 and signal processing device118.

The system 200 may also be used to monitor changes in frequency ofdynamic strain in the wellbore 234. Alternatively, or additionally, thesystem 200 may be used to monitor changes in magnitude of dynamic strainof the housing. A change in magnitude of dynamic strain may indicatestretch, compression, elongation or shear of the production tubing 220or casing 216, 218. The magnitude of dynamic strain may also indicateseverity of the strain being applied to the production tubing 220 orcasing 216, 218, for example, the larger the strain being applied to theproduction tubing 220 or casing 216, 218, the greater the magnitude ofdynamic strain. It follows that the more severe the strain being appliedat a particular location of the production tubing 220 or casing 216,218, the more likely the production tubing 220 or casing 216, 218 willbe compromised and fail in the future. The system 200 may be used tomonitor cumulative strain in the wellbore 234 over time.

It is contemplated that any part of any aspect or embodiment discussedin this specification can be implemented or combined with any part ofany other aspect or embodiment discussed in this specification.

For the sake of convenience, the exemplary embodiments above aredescribed as various interconnected functional blocks. This is notnecessary, however, and there may be cases where these functional blocksare equivalently aggregated into a single logic device, program oroperation with unclear boundaries. In any event, the functional blockscan be implemented by themselves, or in combination with other pieces ofhardware or software.

While particular embodiments have been described in the foregoing, it isto be understood that other embodiments are possible and are intended tobe included herein. It will be clear to any person skilled in the artthat modifications of and adjustments to the foregoing embodiments, notshown, are possible.

1. (canceled)
 2. A cumulative strain monitoring method comprising: (a)shining laser light along an optical fiber to detect dynamic strain of ahousing, wherein the optical fiber comprises at least one pair of fiberBragg gratings (FBGs) tuned to reflect substantially identicalwavelengths with a first segment of the optical fiber extending entirelylinearly between the at least one pair of FBGs; (b) detecting lightreflected by the at least one pair of FBGs and performing interferometryon the reflected light to produce dynamic strain measurements based onthe interferometry; (c) monitoring the dynamic strain measurements overtime; and (d) producing a cumulative dynamic strain measurement from themonitored dynamic strain measurements.
 3. The method of claim 2, whereinshining the laser light comprises shining a reference light pulse and asensing light pulse along the optical fiber, the reference light pulsebeing delayed compared to the sensing light pulse by a predeterminedperiod of time selected such that the reference light pulse reflected bya first FBG of the at least one pair of FBGs interferes with the sensinglight pulse reflected by a second FBG of the at least one pair of FBGsto form a combined interference pulse, and wherein detecting the lightreflected by the at least one pair of FBGs and performing theinterferometry comprise detecting the combined interference pulse anddetecting a phase difference between the reflected reference light pulseand the reflected sensing light pulse of the combined interference pulseto produce the dynamic strain measurements.
 4. The method of claim 2,wherein the housing is a pipeline.
 5. The method of claim 2, furthercomprising burying the optical fiber in the ground near the housing. 6.The method of claim 2, wherein the optical fiber is buried between twopipelines and used to monitor the dynamic strain of both pipelines. 7.The method of claim 2, wherein different pairs of the at least one pairof FBGs respectively correspond to different sensor zones, and whereinthe dynamic strain measurements are monitored and the cumulative dynamicstrain measurement is produced for each of the zones.
 8. The method ofclaim 7, wherein the different pairs are respectively tuned to differentwavelengths and the interferometry is performed using wavelengthdivision multiplexing.
 9. The method of claim 7, wherein the differentpairs are tuned to a first wavelength, and wherein performing theinterferometry comprises shining laser light at the first wavelengthalong the optical fiber and applying time division multiplexing.
 10. Themethod of claim 7, further comprising graphing the cumulative dynamicstrain for the different zones vs. time.
 11. The method of claim 2,further comprising: (a) comparing the cumulative strain to apredetermined reference value; and (b) providing an indication to anoperator to replace the housing.
 12. A cumulative strain monitoringsystem comprising: (a) an optical fiber comprising at least one pair offiber Bragg gratings (FBGs), wherein a first segment of the opticalfiber extends entirely linearly between the at least one pair of FBGsand wherein the at least one pair of FBGs are tuned to reflect a firstwavelength of laser light; (b) an interrogator comprising a laser sourceand a photodetector, wherein the interrogator is configured to performinterferometry based on a phase difference resulting from a change in anoptical path length between a first FBG and a second FBG of the at leastone pair of FBGs by shining laser light at the first wavelength alongthe optical fiber and detecting light reflected by the at least one pairof FBGs, and wherein the interrogator outputs dynamic strainmeasurements based on interferometry performed on the reflected light;and (c) a signal processing device configured to monitor the dynamicstrain measurements over time and to produce a cumulative dynamic strainmeasurement from the monitored dynamic strain measurements.
 13. Thesystem of claim 12, wherein the interrogator is configured to: (a) shinea reference light pulse and a sensing light pulse along the opticalfiber, the reference light pulse being delayed compared to the sensinglight pulse by a predetermined period of time selected such that thereference light pulse reflected by the first FBG of the at least onepair of FBGs interferes with the sensing light pulse reflected by thesecond FBG of the at least one pair of FBGs to form a combinedinterference pulse; (b) detect the combined interference pulse; and (c)detect as the phase difference a difference in phase between thereflected reference light pulse and the reflected sensing light pulse ofthe combined interference pulse to produce the dynamic strainmeasurements.
 14. The system of claim 12, further comprising a firstpipeline and wherein the dynamic strain measurements are of thepipeline.
 15. The system of claim 12, wherein the optical fiber isburied in the ground near the pipeline.
 16. The system of claim 12,further comprising two pipelines and wherein the optical fiber is buriedbetween the two pipelines and used to monitor the dynamic strain of bothpipelines.
 17. The system of claim 12, wherein different pairs of the atleast one pair of FBGs respectively correspond to different sensorzones, and wherein the dynamic strain measurements are monitored and thecumulative dynamic strain measurement is produced for each of the zones.18. The system of claim 17, wherein the different pairs are respectivelytuned to different wavelengths, and the interferometry is performedusing wavelength division multiplexing.
 19. The system of claim 17,wherein the different pairs are tuned to a first wavelength, and whereinperforming the interferometry comprises shining laser light at the firstwavelength along the optical fiber and applying time divisionmultiplexing.
 20. The system of claim 17, further comprising a displayand wherein the signal processing device is further configured to graphthe cumulative dynamic strain for the different zones vs. time on thedisplay.
 21. The system of claim 12, wherein the signal processingdevice is further configured to: (a) compare the cumulative strain to apredetermined reference value; and (b) provide an indication to anoperator to replace the housing.